| nr |
titel |
auteur |
tijdschrift |
jaar |
jaarg. |
afl. |
pagina('s) |
type |
| 1 |
Actor-critic-based predefined-time control for spacecraft attitude formation system with guaranteeing prescribed performance on SO(3)
|
Shi, Xiao-Ning
|
|
|
117 |
C |
p.
|
artikel
|
| 2 |
Adaptive prescribed performance attitude control for RLV with mismatched disturbance
|
Tian, Bailing
|
|
|
117 |
C |
p.
|
artikel
|
| 3 |
A 3D implicit structured multi-block grid finite volume method for computational structural dynamics
|
Ma, Li
|
|
|
117 |
C |
p.
|
artikel
|
| 4 |
A DoE-based approach for the implementation of structural surrogate models in the early stage design of box-wing aircraft
|
Cipolla, V.
|
|
|
117 |
C |
p.
|
artikel
|
| 5 |
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
|
Li, Mengzhe
|
|
|
117 |
C |
p.
|
artikel
|
| 6 |
Aeroelastic stability and nonlinear flutter analysis of viscoelastic heated panel in shock-dominated flows
|
Ye, Liu-qing
|
|
|
117 |
C |
p.
|
artikel
|
| 7 |
A low-loss vector exhaust guide vanes and its application
|
Zhou, Yang
|
|
|
117 |
C |
p.
|
artikel
|
| 8 |
An adaptive Sequential Enhanced PCE approach and its application in aerodynamic uncertainty quantification
|
Zhang, Wei
|
|
|
117 |
C |
p.
|
artikel
|
| 9 |
An experimental investigation on damage mechanisms of thick hybrid composite structures under flexural loading using multi-instrument measurements
|
Gul, S.
|
|
|
117 |
C |
p.
|
artikel
|
| 10 |
An investigation on winglet design with limited computational cost, using an efficient optimization method
|
Heidari Soreshjani, Masoud
|
|
|
117 |
C |
p.
|
artikel
|
| 11 |
A novel preliminary design method for intermediate compressor/turbine ducts
|
Yang, Jinguang
|
|
|
117 |
C |
p.
|
artikel
|
| 12 |
Application and implementation of the bond graph methodology on the structural damage detection and monitoring of aeroengines
|
Mir-Haidari, Seyed-Ehsan
|
|
|
117 |
C |
p.
|
artikel
|
| 13 |
Comparison of different plasma actuation strategies for aeroelastic control on a linear compressor cascade
|
De Giorgi, Maria Grazia
|
|
|
117 |
C |
p.
|
artikel
|
| 14 |
Corrigendum to “Spark ignition and stability limits of spray kerosene flames under subatmospheric pressure conditions” [Aerosp. Sci. Technol. 114 (2021) 106734]
|
Huang, Yakun
|
|
|
117 |
C |
p.
|
artikel
|
| 15 |
Design of a Mach 2 shape transition nozzle for lab-scale direct-connect supersonic combustor
|
Sung, Bu-Kyeng
|
|
|
117 |
C |
p.
|
artikel
|
| 16 |
Displacement field reconstruction of structures under thermal and mechanical loading environment
|
Wang, Xiaojun
|
|
|
117 |
C |
p.
|
artikel
|
| 17 |
Distributed adaptive cooperative time-varying formation tracking guidance for multiple aerial vehicles system
|
Yu, Jianglong
|
|
|
117 |
C |
p.
|
artikel
|
| 18 |
Distributed fusion in harsh environments using multiple bearings-only sensors with out-of-sequence-refined measurements
|
Shi, Yifang
|
|
|
117 |
C |
p.
|
artikel
|
| 19 |
Editorial Board
|
|
|
|
117 |
C |
p.
|
artikel
|
| 20 |
Effect of fill flow rate on flame acceleration in a detonation channel
|
Wang, Yun
|
|
|
117 |
C |
p.
|
artikel
|
| 21 |
Effects of compressible flow phenomena on aerodynamic characteristics in Hyperloop system
|
Jang, Kyeong Sik
|
|
|
117 |
C |
p.
|
artikel
|
| 22 |
Evaluation of applicability of empirical models of turbine performance to aircraft engine
|
Sun, Penghui
|
|
|
117 |
C |
p.
|
artikel
|
| 23 |
Evaluation of the two-γ model and the energy balance process of a Chapman-Jouguet detonation
|
Li, Qingan
|
|
|
117 |
C |
p.
|
artikel
|
| 24 |
Event-based distributed bias compensation pseudomeasurement information filter for 3D bearing-only target tracking
|
Wang, Yu
|
|
|
117 |
C |
p.
|
artikel
|
| 25 |
Event-triggered anti-disturbance attitude and vibration control for T-S fuzzy flexible spacecraft model with multiple disturbances
|
Wang, Yawen
|
|
|
117 |
C |
p.
|
artikel
|
| 26 |
Experimental investigation of serpentine nozzles for turbofan
|
Hui, Zhonghao
|
|
|
117 |
C |
p.
|
artikel
|
| 27 |
Experimental study on the temperature and structure of the exhaust plume in valveless pulse detonation engines
|
Wang, Zhiwu
|
|
|
117 |
C |
p.
|
artikel
|
| 28 |
Experimental validation of a new type of direct-connect facility for scramjet studies
|
Guan, Ruiqing
|
|
|
117 |
C |
p.
|
artikel
|
| 29 |
Flow mechanism of bimodal phenomenon in intermittent corner separation in a linear compressor cascade using a hybrid RANS/LES method
|
Lu, Bingxiao
|
|
|
117 |
C |
p.
|
artikel
|
| 30 |
Flow simulation of a supersonic airplane with installed engine nacelle
|
Kim, Hyoungjin
|
|
|
117 |
C |
p.
|
artikel
|
| 31 |
Geometrically nonlinear aeroelastic characteristics of highly flexible wing fabricated by additive manufacturing
|
Tsushima, Natsuki
|
|
|
117 |
C |
p.
|
artikel
|
| 32 |
Guided wave-hidden Markov model for on-line crack evaluation of a full-scale aircraft
|
Zhang, Jinjin
|
|
|
117 |
C |
p.
|
artikel
|
| 33 |
Gust load alleviation by normal microjet
|
Li, Yonghong
|
|
|
117 |
C |
p.
|
artikel
|
| 34 |
Historical development and use of CFD for separated flow simulations relevant to military aircraft
|
Rizzi, Arthur
|
|
|
117 |
C |
p.
|
artikel
|
| 35 |
Hovering efficiency optimization of the ducted propeller with weight penalty taken into account
|
Hu, Yu
|
|
|
117 |
C |
p.
|
artikel
|
| 36 |
Hybrid control of a satellite with membrane antenna considering nonlinear vibration
|
Liu, Xiang
|
|
|
117 |
C |
p.
|
artikel
|
| 37 |
Ignition enhancement of lean kerosene air mixture by multichannel jet enhanced plasma igniter
|
Miao, Huifeng
|
|
|
117 |
C |
p.
|
artikel
|
| 38 |
Improved high-degree cubature Kalman filter based on resampling-free sigma-point update framework and its application for inertial navigation system-based integrated navigation
|
Cui, Bingbo
|
|
|
117 |
C |
p.
|
artikel
|
| 39 |
Inertia-free appointed-time prescribed performance tracking control for space manipulator
|
Fan, Yidi
|
|
|
117 |
C |
p.
|
artikel
|
| 40 |
Influence of circumferential grooves on the aerodynamic and aeroelastic stabilities of a transonic fan
|
Cong, Jiqing
|
|
|
117 |
C |
p.
|
artikel
|
| 41 |
Inhomogeneous behavior of supercritical hydrocarbon fuel flow in a regenerative cooling channel for a scramjet engine
|
Sun, Feng
|
|
|
117 |
C |
p.
|
artikel
|
| 42 |
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation
|
Yang, Lei
|
|
|
117 |
C |
p.
|
artikel
|
| 43 |
Low-cost MIMU based AMS of highly dynamic fixed-wing UAV by maneuvering acceleration compensation and AMCF
|
Guan, Lianwu
|
|
|
117 |
C |
p.
|
artikel
|
| 44 |
Modified spiral folding pattern for deployable membranes
|
Liyanage, P.M.
|
|
|
117 |
C |
p.
|
artikel
|
| 45 |
Motion and dynamic analyses of a human centrifuge system with an efficient design configuration
|
Mohajer, Navid
|
|
|
117 |
C |
p.
|
artikel
|
| 46 |
Multiple-model adaptive control architecture for a quadrotor with constant unknown mass and inertia
|
Outeiro, Pedro
|
|
|
117 |
C |
p.
|
artikel
|
| 47 |
Non-axisymmetric aero-engine nacelle design by surrogate-based methods
|
Tejero, Fernando
|
|
|
117 |
C |
p.
|
artikel
|
| 48 |
Novel Omnimagnet actuation method for a Cubesat nano-satellite
|
Hassan, Amr M.
|
|
|
117 |
C |
p.
|
artikel
|
| 49 |
Numerical study on the trajectory of a long-range flexible rocket with large slenderness ratio
|
Wang, Yabin
|
|
|
117 |
C |
p.
|
artikel
|
| 50 |
Online-learning control with weakened saturation response to attitude tracking: A variable learning intensity approach
|
Zhang, Chengxi
|
|
|
117 |
C |
p.
|
artikel
|
| 51 |
Optimal drag-energy entry guidance via pseudospectral convex optimization
|
Sagliano, Marco
|
|
|
117 |
C |
p.
|
artikel
|
| 52 |
Overall and component basis performance evaluations for turbojet engines under various optimal operating conditions
|
Fawal, Sara
|
|
|
117 |
C |
p.
|
artikel
|
| 53 |
Parametric study of aerodynamic performance of equivalent ducted/un-ducted rotors
|
Zhang, T.
|
|
|
117 |
C |
p.
|
artikel
|
| 54 |
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
|
Yao, Wei
|
|
|
117 |
C |
p.
|
artikel
|
| 55 |
Performance augmentation mechanism of tandem flapping foils with stroke time-asymmetry
|
Wang, Guangjian
|
|
|
117 |
C |
p.
|
artikel
|
| 56 |
Performance evaluation for scramjet based on ground direct-connected test: A method investigation
|
Li, Chaolong
|
|
|
117 |
C |
p.
|
artikel
|
| 57 |
Planning and distributed control for cooperative transportation of a non-uniform slung-load by multiple quadrotors
|
Arab, Farhad
|
|
|
117 |
C |
p.
|
artikel
|
| 58 |
Predicting high-speed feedback mechanisms in rectangular cavities using lattice-Boltzmann very-large eddy simulations
|
Mancini, Simone
|
|
|
117 |
C |
p.
|
artikel
|
| 59 |
Predictor-based pose stabilization control for unmanned vehicles on SE(3) with actuator delay and saturation
|
Peng, Xiuhui
|
|
|
117 |
C |
p.
|
artikel
|
| 60 |
Preliminary study on pulsed jets with three-dimensional effects for flow separation control in a compressor blade
|
Lu, Weiyu
|
|
|
117 |
C |
p.
|
artikel
|
| 61 |
PyVT: A python-based open-source software for visualization and graphic analysis of fluid dynamics datasets
|
Liu, Qing
|
|
|
117 |
C |
p.
|
artikel
|
| 62 |
Quasi-static numerical simulation of the dynamic launching process for high-altitude balloon
|
Zhang, Hangyue
|
|
|
117 |
C |
p.
|
artikel
|
| 63 |
Rapid algorithm for covariance ellipsoid model based collision warning of space objects
|
Han, Chao
|
|
|
117 |
C |
p.
|
artikel
|
| 64 |
Rapid search method for a spacecraft attitude maneuver path with multiple constraints
|
Wang, Zhuo
|
|
|
117 |
C |
p.
|
artikel
|
| 65 |
Recovery trajectory planning for the reusable launch vehicle
|
Cheng, Guanghui
|
|
|
117 |
C |
p.
|
artikel
|
| 66 |
Robust modification of nonlinear L1 adaptive flight control system via noise attenuation
|
Feng, Yue
|
|
|
117 |
C |
p.
|
artikel
|
| 67 |
Scale effect of gas injection into a supersonic crossflow
|
Liang, Changhai
|
|
|
117 |
C |
p.
|
artikel
|
| 68 |
Segmented sliding mode control-based CubeSat rapid attitude manoeuvre in low magnetic environment
|
Zhang, Xiaohua
|
|
|
117 |
C |
p.
|
artikel
|
| 69 |
Shape and envelope tension prediction of natural shaped high altitude balloons
|
Liao, Jun
|
|
|
117 |
C |
p.
|
artikel
|
| 70 |
Shock dynamics and expansion characteristics of an aerospike nozzle and its interaction with the rotating detonation combustor
|
Huang, Yue
|
|
|
117 |
C |
p.
|
artikel
|
| 71 |
Software-in-the-loop investigation of wake-vortex-encounter-response of identical multirotor pair with PX4 attitude controller
|
Wang, C.H. John
|
|
|
117 |
C |
p.
|
artikel
|
| 72 |
Spatial correlation effect of a multidimensional force on vibration suppression
|
Zhao, XiaoJian
|
|
|
117 |
C |
p.
|
artikel
|
| 73 |
Spatial path analysis for high-altitude solar-powered airship with maximum net energy
|
Zhu, Weiyu
|
|
|
117 |
C |
p.
|
artikel
|
| 74 |
The formation and development of oblique detonation wave with different chemical reaction models
|
Guo, Hongbo
|
|
|
117 |
C |
p.
|
artikel
|
| 75 |
Trajectory optimization-based maneuverability assessment of eVTOL aircraft
|
Wang, Mingkai
|
|
|
117 |
C |
p.
|
artikel
|
Tijdschrift beschrijving